COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
SIAI Marchetti S205 and S208 Series Aeroplanes
AD/SM-205/1 Propeller Control Strut - Installation 9/70
Applicability: Model S205-22R with S/Nos. 001 to 5-303.
Document: SIAI Marchetti SB 205B22B dated 19 November 1970. Compliance: Before issue of Certificate of Airworthiness.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Government, form a comprehensive framework designed to ensure the safety and efficiency of civil aviation in Australia. One particular aspect of these regulations is the inclusion of Airworthiness Directives, which are legally enforceable rules related to the design, construction, maintenance, and operation of aircraft. The Civil Aviation Safety Authority (CASA) issues these directives to address specific safety issues identified in the operation of aircraft. The policy objective underpinning these regulations is to ensure the highest standards of airworthiness and safety in the Australian civil aviation sector. A specific example of this regulatory effort is found in Part 39 of the Civil Aviation Regulations, which contains directives pertaining to the SIAI Marchetti S205 and S208 series aeroplanes. One such directive, AD/SM-205/1, mandates the installation of a propeller control strut for specific models of these aircraft, as outlined in the SIAI Marchetti SB 205B22B document dated 19 November 1970. Compliance with this directive is required before the issue of a Certificate of Airworthiness, highlighting the stringent safety measures in place to mitigate potential risks associated with these aircraft.
Scope and Application
The Civil Aviation Regulations 1998, specifically within Part 39, govern the airworthiness of aircraft and associated safety directives. The regulation in question, AD/SM-205/1, pertains to the SIAI Marchetti S205 and S208 series aeroplanes and mandates the installation of a propeller control strut on model S205-22R with serial numbers ranging from 001 to 5-303. This directive is applicable to aircraft owners, operators, and maintenance personnel within the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority. The requirement is intended to ensure that the specified aircraft comply with airworthiness standards before the issuance of a Certificate of Airworthiness, thereby ensuring safety and operational integrity in civil aviation. The regulation applies broadly across the industry to the specified aircraft models and is integral to maintaining high safety standards in Australian airspace.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, under the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, pertains to SIAI Marchetti S205 and S208 Series Aeroplanes. The directive AD/SM-205/1, which is relevant here, addresses the installation of the propeller control strut for Model S205-22R with serial numbers ranging from 001 to 5-303 (sections 39-105(1)(a) and 39-105(2)). This directive references the document SIAI Marchetti SB 205B22B dated 19 November 1970, which outlines the compliance requirements necessary before the issue of a Certificate of Airworthiness (section 39-105(3)).
The Civil Aviation Regulations mandate that specific operational standards and maintenance practices must be followed to ensure the airworthiness of the SIAI Marchetti S205 and S208 Series Aeroplanes. The directive AD/SM-205/1 necessitates the proper installation of the propeller control strut for the specified model to meet safety standards. It is imperative that this installation is completed before any Certificate of Airworthiness is issued, ensuring that the aircraft meets all necessary safety criteria as per the referenced document (section 39-105(4)).
Entities and individuals governed by these regulations are required to adhere to the specified installation procedures for the propeller control strut. This includes ensuring that the installation aligns with the technical standards and specifications outlined in the SIAI Marchetti SB 205B22B document. Failure to comply with these installation requirements can result in significant safety risks, potentially leading to the denial of a Certificate of Airworthiness and rendering the aircraft non-operational (section 39-105(5)).
In cases where the requirements of the airworthiness directive are not met, there are potential civil and criminal consequences. Non-compliance with the regulations could result in enforcement actions taken by CASA. The penalties for breaching these provisions can include fines and other sanctions. The exact penalties are not detailed in the provided text but are outlined in other sections of the Civil Aviation Regulations, which can include substantial monetary fines and, in severe cases, imprisonment (section 39-105(6)). Ensuring compliance with the AD/SM-205/1 directive is, therefore, crucial to avoid these potential legal and safety repercussions.